Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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Ambient air at 100 kPa and 300 K is compressed isentropically in a steady-flow device to 0.8 MPa. Determine the work input to the compressor.
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- Required information Problem 07.088 - DEPENDENT MULTI-PART PROBLEM - ASSIGN ALL PARTS NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Air is compressed in a piston-cylinder device from 90 kPa and 20°C to 450 kPa in a reversible isothermal process. Problem 07.088.b - Work done during the process Determine the work done. The work done is kJ/kg.arrow_forwardAir enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 °Cwith a low velocity and exits at 1 MPa and 347 C with a velocity of 90 m/s. The compressionprocess is adiabatic, and the power input is 200. Determine the mass flowrateof the air through the compressor.arrow_forwardAir enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰Cwith a low velocity and exits at 2 MPa and 350 ⁰C with a velocity of 140 m/s. Thecompression process is adiabatic, and the power input is 240. Determine the massflowrate of the air through the compressor.arrow_forward
- Answer in box is incorrectarrow_forwardPropane initially at 300 K and 100 kPa is is compressed to 1 MPa in a reversible, steady-flow, and compressor. Determine the amount of work in kJ/kg if the process is isothermal. Round your answer to one decimal placearrow_forwardA steady-flow compressor has R-134a entering at 120 kPa as a saturated vapor and exits at 800 kPa and 50°C, requiring 55 kJ/kg of work. Assume that the boundary of the compressor is at 30°C. What is the specific enthalpy of the R-134a at the inlet, in kJ/kg? What is the specific enthalpy of the R-134a at the outlet, in kJ/kg? How much heat transfer, in kJ/kg, exits the system?arrow_forward
- Air is compressed in an adiabatic compressor. Inlet and outlet conditions are 120kPa, 30 oC and 20 m/s; 1.4 MPa, 530 oC and 80 m/s. The surrounding air temperature is 25 oC. The inlet cross-sectional area is 0.013 m2. Assume Cp = 1005 J/kgK, R = 287 J/kgK, k = 1.4. Enter the amount of heat loss due to irreversibility resulting from the heat transfer from the compressor in kW (correct up to one decimal place.)arrow_forwardCalculate the axial stress in a tube that is stretched by a tensile axial force of 4500 N if the tube has an outer diameter of 25 mm and an inner diameter of 20 mm.arrow_forward
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